Field of invention
[0001] This invention relates to a pump in which suction is achieved by interaction between
a working liquid and an orifice. Such pumps may be used for either evacuating fluids
from or compressing fluids into closed spaces.
[0002] The term fluid as used herein means a fluid which is less dense than the working
liquid utilised in the pump, and may be a gas or gaseous mixture such as air.
[0003] In pumps of this type, where the fluid is a gas, a degree of mixing (as by dissolving
or limited entrainment of gas bubbles) may be acceptable. However where liquids are
concerned they should not in general be totally miscible.
Background to the invention and prior art
[0004] US Patent 3384023 describes an example of such a pump in which a liquid annulus is
created by rotating a housing (26) within which is mounted a stationary disc (32)
carrying four velocity tubes (50), each of which includes a venturi restriction (56).
In each velocity tube there is an enlarged cavity (64) to the rear of the venturi
restriction (56) and the cavity communicates with a passage (54). As the working liquid
is rotated past each velocity tube (50) some of the liquid passes into the tube and
on passing axially through the venturi restriction reduces the pressure within the
cavity (64) behind the restriction due to volume changes within the tube. This causes
fluid to be drawn through the the passage (54) and into the velocity tube for discharge
through the end (62).
[0005] Other velocity tube devices are indicated as being usable, operating on an aspirator
or jet pump principle, in place of the described nozzle-venturi combination.
[0006] Examples given are:
(1) a simple venturi tube with the suction tube (54) connected to the throat of the
venturi restriction, and;
(2) a tube incorporating an internal pitot tube connected to the suction tube (54).
[0007] However, all the described pumps employ suction producing devices in which the suction
producing orifice is located in an internal surface of the device and suction is only
achieved by causing the working liquid to pass through the device. Since the suction
effect is related to flow rate and volume, the pumping speed (ie. throughput) is severely
limited due to the small flows which such velocity tube devices can accommodate.
[0008] The present invention on the other hand is concerned with a pump which whilst utilizing
the interaction between a working liquid and an orifice to provide a suction effect
on a fluid, does not require the working liquid to flow through an orifice to obtain
the suction effect. The pump of the present invention does not therefore suffer the
same pumping speed restrictions as the prior art designs do and is thereby capable
of greatly increased performance and throughput.
Summary of invention
[0009] According to the present invention, there is provided a pump comprising:
- a pump housing having a generally cylindrical interior and enclosing a quantity
of working liquid,
- at least one probe having at least one aperture on its exterior surface and internal
passage means for communicating said aperture with a first external space,
- means for causing the working liquid to move in a circular path inside the housing
and relative to and past the aperture in the probe, and
- outlet means for communicating between a second external space and a central region
of the housing which in use is free of working liquid,
whereby fluid to be pumped is drawn from the said first external space, through the
aperture in the exterior surface of the probe, to pass as fluid bubbles towards the
central region of the housing as a result of centrifugal forces acting on the more
dense working liquid, the bubbles migrating through the circulating liquid into the
central region to pass out of the housing through the outlet means.
[0010] The aperture in the external surface of the probe can (assuming the probe to be of
sufficient width) be extended so as to co-act with liquid across substantially the
whole of the width of the pump housing, thereby increasing the pumping speed.
[0011] The term 'generally cylindrical' is used in this specification to include housing
interiors which depart to some degree from perfect cylindricality, and which may for
example be slightly ellipsoidal or oval or which have irregularities in their internal
walls and is intended also to include a tapering cylinder.
[0012] The pump will generally comprise relatively rotating inner and outer parts, one carrying
the probe or probes and the otner causing the working liquid to move in its circular
path.
[0013] In one embodiment, the pump housing forms the stator of the pump and carries the
probe or probes, whilst the rotor is formed by the circulating liquid. Because the
rotor is a mass of liquid, it automatically forms the necessary seal between the rotor
and the stator, and additionally no lubrication is required as would be required between
a solid rotor and a solid stator.
[0014] In one embodiment the means for causing the liquid to move in a circular path is
an impeller (constituting the inner part of the pump) mounted coaxially within the
housing and having radially-extending blades which extend into the liquid flow path.
The blades do not need to, and should not, extend into contact with the pump housing.
[0015] In an alternative embodiment, the pump housing rotates about a central hub constituting
the inner part of the pump, and the rotation of the housing produces the desired circular
movement of the liquid. The probe or probes can then be mounted on the central hub
so that it or they project radially from the hub into the flow path.
[0016] According to an important feature of the invention, the part of the pump not carrying
the probe or probes, preferably the housing, carries angularly spaced protrusions.
[0017] It is believed that it is necessary for the said protrusions to pass sufficiently
close to the probe or probes to cause short burst of acceleration of the region of
liquid local to each probe, as the liquid is squeezed between the probe and the protrusion
passing thereby, in order to enhance suction at the probe aperture.
[0018] Most preferably, the spacing apart and the individual shapes of the protrusions and
their spacing from each probe is optimised to maximise the flow of fluid drawn through
the probe as a result of the acceleration of the liquid past the aperture(s) for a
given power input for driving the relatively rotating parts of the pump.
[0019] Each probe can be in the form of a tube having a closed end with the aperture in
a side wall of the tube.
[0020] The tube may be circular in cross-section or may have a triangular cross-sectional
shape or may be of a more flattened streamlined cross-sectional shape, although it
is anticipated that other probe shapes could alternatively be used, including shapes
chosen to minimise the hyrdrodynamic drag exerted on the liquid rotor by the probe.
[0021] In a particularly preferred design the probe is in the form of a wing extending parallel
to the pump axis, and supported on a strut attached to the hub.
[0022] Alternatively, in a preferred embodiment, the or each probe such as a wing is supported
by a disc located within the pump housing, the latter constituting the rotating part
of the pump.
[0023] Preferably, the faces of the stationary supporting disc are narrowly spaced from
respective rotating plate surfaces wherein thin liquid films are contained. Thus,
in one instance, one face of the supporting disc is spaced from one end face of the
housing by one said liquid film and the other face of the disc is spaced by another
said liquid film from a guard disc mounted to rotate with the housing. The mounting
of the guard disc is apertured to provide for passage of fluid to the central region
of the housing.
[0024] However, a centrally located supporting disc with a guard disc on each side thereof
is also possible.
[0025] Both the inlet to and the outlet from the pump may pass through the hub.
[0026] Where a circular cross section tubular probe extends radially within the housing
it is found that the aperture should face in a direction substantially perpendicular
to the general direction of flow relative to the probe. (ie the aperture axis should
be substantially perpendicular to the direction of flow).
[0027] If such a circular cross section probe extends axially parallel to the axis of the
cylindrical interior of the housing at a position remote from the said axis, the aperture
is again advantageously orientated so as to face in a direction substantially perpendicular
to the general direction of liquid flow relative to the probe. This may be either
so as to face radially inwardly or radially outwardly.
[0028] By "substantially perpendicular" is meant that the aperture axis subtends an angle
to the general direction of liquid flow in the range 45° to 120°, typically 50° to
90°. These ranges are based on empirical observations and it is possible that wider
or different ranges may be appropriate depending on further experimental work.
[0029] Positioning the aperture so that its axis is substantially perpendicular to the direction
of flow produces a substantial suction effect through the probe, which enables the
pump to function. Fluid such as air or gas, sucked in through the probe, passes towards
the central region of the housing as a result of centrifugal forces acting on the
more dense liquid, and thereby migrates through the liquid flow into the cylindrical
space of the housing, from where it can escape.
[0030] If a probe has a wing cross-section, the aperture is preferably located in a part
of the wing surface at which a region of low pressure is created during fluid flow.
As with the cylindrical tubular probe, the wing may be located in the housing so that
the cross-section of the wing extends generally radially or generally parallel to
the axis of the cylindrical housing.
[0031] One preferred wing profile has a shape affording a ramp surface at the leading edge
of the wing, preceding the aperture. The ramp may be linear or convexly or concavely
curved. The aperture is preferably disposed at the top of the ramp. The downstream
wing surface may also be in the form of a ramp which may be linear but more probably
is convexly curved so as to maximise the suction effect whilst minimising drag.
[0032] Where appropriate, valve means such as for example a one way valve, may be provided
in the fluid path to the probe aperture and other such valve means may be provided
in the outlet means from the housing.
[0033] The liquid used can be chosen according to the particular application and may include
water or oil or liquid metals although this list is not intended to be exhaustive.
[0034] When used as a vacuum pump, where a high vacuum is required and clean gases are being
pumped, a vacuum oil or fluid would typically be used. A low melting point liquid
metal or metal alloy such as an indium gallium tin eutectic may be employed when total
absence of hydrocarbons is required.
[0035] Where the liquid becomes contaminated in use, means may be provided for replacing
the liquid or filtering same.
[0036] Water can be used as the working liquid for compressing gases such as air and for
evacuating if only a moderate vacuum is required.
[0037] Where a fluid to be pumped is chemically aggressive and the pump requires any sealing
liquids also to have lubricating properties, it is often difficult and usually expensive
to find an appropriate chemically inert substance. However, a pump constructed in
accordance with the present invention requires no lubrication as such 'in the pumping
chamber. There is therefore no requirement for the working liquid to have lubricating
properties in the working area of the pump, and therefore there is a greater choice
of liquids available.
[0038] If a magnetic or magnetisable or electrically conductive liquid is employed such
as for example a liquid metal or liquid metal alloy, the rotation of this liquid relative
to the probe or probes may be effected by influencing the liquid with a rotating magnetic
field, in which event the housing may remain stationary or be rotated. The material
forming the housing must not impede or screen the magnetic field if this is established
by external means such as a coil.
[0039] It has also been found that where a wing with a leading edge ramp profile is employed,
the pumping speed (ie throughput) can be increased by providing one or more disturbance
bars in the form of ridges or protrusions on the surface of the ramp, so as to introduce
a rough surface effect on the ramp. It is believed that this increases the turbulance
in the region of the aperture and this increases the suction effect.
Brief description of the drawings
[0040] The invention will now be further described, by way of example, with reference to
the accompanying drawings in which:
Figure 1 is a transverse cross-section through a pump constructed as a first embodiment
of the invention;
Figure 2 is a cross-section through a pump constructed as a second embodiment of the
invention;
Figure 3 shows a modification to the second embodiment;
Figure 4 is a cut-away view showing the second embodiment with a minor modification;
Figure 5 shows a preferred embodiment in axial cross-section; and
Figure 6 shows a modification of the embodiment of Figure 5.
Description of embodiments
[0041] The pumps shown in the drawings can be used either to evacuate or partially evacuate
an enclosure connected to the input so as to produce a vacuum, or can be used to compress
fluid, especially air or gas, into a chamber connected to the output. As shown the
pumps are intended to operate as vacuum pumps.
[0042] The pump shown in Figure 1 has a cylindrical housing 10, and a tubular probe 12 extending
through the housing wall.
[0043] Within the housing is a body of liquid 14. In the Figure, this body of liquid is
shown in the position which it will take up when the pump is in use, ie. when the
body of liquid has a high circular speed of rotation causing the liquid to be forced
out against the housing walls.
[0044] Mounted coaxially within the housing is an impeller 16 which has a central core 18
and a number of radial blades 20. An external motor (such as shown in part in Fig
4) will drive the impeller 16 in rotation and the rotating blades 20 will act on the
liquid 14 to set this in motion. Thus the rotating impeller 16 will cause the liquid
to move in its circular path, and this will result in a cylindrical space 24 at the
centre of the housing being free of liquid during operation. Since the pump is intended
to operate as a vacuum pump outlet 26 extends from the space 24 to atmosphere, and
when the pressure in the space 24 builds up above atmospheric, the excess pressure
is dissipated through the outlet 26. Where a flow control valve such as a one-way
valve is to be incorporated in the inlet or the outlet or both it may be located at
equivalent positions such as are shown in Figure 2.
[0045] In the case of a multistage pump, the outlet 26 will be connected to the inlet of
the next stage of the pump.
[0046] The probe 12 shown is in the form of a cylindrical tube and this tube will be connected
to the space to be evacuated. Near the bottom of the tube is an opening in the tube
side wall. The end of the tube is closed. As shown, this opening 28 is open in a direction
generally prpendicular to the flow of liquid indicated by the arrows 30. As the body
of liquid 14 rotates, air or gas is drawn through the tubular probe 12 through the
opening 28 and into the body of liquid. From there, the fluid (such as air or gas)
which is now in the form of bubbles, migrates into the central space 24 and escapes
through the outlet 26.
[0047] More than one tubular prcbe 12 may be located around the cylindrical housing to provide
separate independent pumping devices or if connected in parallel to increase the pumping
speed or throughput.
[0048] The pump shown in Figure 2 also has a housing 10 which is set in rotation in the
direction of arrows 42 by an external motor (not shown in the Figure but which would
be similar to that shown in part in Figure 4). The housing rotates about a central
hub 44. As in the embodiment of Figure 1, a body of liquid 46 is shown in the position
it will take up when in use.
[0049] Radial protrusions 48 are provided around the inner surface of the housing 10. These
protrusions help to set the liquid 46 in motion when the housing rotates, but also
serve another important purpose, as later described.
[0050] The protrusions 48 may extend parallel to the axis of the housing or may be skewed
relative thereto.
[0051] A stem 50 (preferably streamlined in shape) extends radially from the hub 44 and
carries a probe 52 which is located within the flowing liquid 46. The probe is wing
shaped and is aligned with the liquid flow direction and extends nearly the full length
of the cylinder. A suction passage 54 opens in the radially outer surface of the probe
and may be a circular hole 56 (or holes) or preferably a slot parallel to the pump
axis.
[0052] An exhaust passage 58 opens into the cylindrical space 60 at the centre of the pump,
and both passages 54 and 58. pass out of the pump through the central hub 44.
[0053] When employed to compress air (or a gas), the chamber into which the air or gas is
to be pumped is connected to the exhaust passage 26 in Figure 1 (58 in Figure 2) and
the inlet 12 in Figure 1 (54 in Figure 2) is left to communicate with atmosphere (in
the case of a straightforward air compression) or to the source of gas (where the
pump is being employed to compress a specific gas). References 52 and 55 denote the
possible positions for flow control valves such as one way valves, if either or both
is required, in the Figure 2 embodiment.
[0054] The liquid 14 or 56 may, in use of the pump for evacuation or for compression purposes,
be oil or possibly water or, if hydrocarbon absence is essential, a low melting point
liquid metal or alloy.
[0055] As with the Figure 1 embodiment, more than one probe and stem assembly such as 50,
52 may be mounted to extend radially from the hub 44, so as to be circularly spaced
around the housing.
[0056] Figure 3 shows a modification of the probe 52 of Figure 2. In this modification,
the probe 70 carried by stem 50 has a basic wing shape based on an axis which is curved.
[0057] The basic wing shape 74 is, however, cut away to form a linear ramp 76 on the leading
side of the wing. The aperture 78, corresponding to the aperture 56 of Figure 2, lies
at the top of this linear ramp 76. The ramp may alternatively be convexly of concavely
curved.
[0058] Filters and/or valve means may be employed in the inlet and outlet as required, as
exemplified by the previously referred to valves 53 and 55.
[0059] In another and possibly preferred modification (see Figure 4), the underside of the
wing 70 is a planar surface, which at least in some circumstances can reduce drag.
[0060] Figure 4 shows the pump of Figure 2 in a cut-away view, with the modification that
the radial protrusions 48 on the interior of the housing 10 are in the form of hemicylindrical
ribs. The wing 70 can be seen to be supported from the hub 44 on two radial struts
79. This wing has a linear ramp surface 76 with an elongate aperture 79 at the top
thereof, and downstream of the ramp has a convexly curved surface 74. The undersurface
80 of the wing is planar.
[0061] Further refinements shown in Figure 4 comprise the inclusion of a disturbance bar
or ridge 81 accross the width of the surface of the ramp 76. More than one such ridge
may be included. Also shown at 77 is part of a winding through which electric current
can be passed to produce a rotating magnetic field for circulating the liquid if the
latter is magnetic or conductive. Also shown at 83 is an electric motor housing for
driving the housing 10. The magnetic and electric motor drives may be used exclusively
or may be used in conjunction.
[0062] Although the struts 79 are shown as having blunt square leading edges, these would
in practice be tapered or streamlined to reduce drag.
[0063] A most important feature of the pump concerns the spacing of the radial protrusions
48 from the wing-shaped probe 70, and in particular from the approximately radially
directed elongate aperture 78 thereof at the top of the linear ramp 76.
[0064] This spacing is sufficiently small to produce a squeezing of the local region of
the working liquid 14 in use, as each protrusion 48 passes the probe 70. The resulting
burst of acceleration of the liquid, in said local region, enhances the suction effect
at the aperture 78, especially in the presence of the ramp surface 74.
[0065] It is especially important to note that increasing the speed of rotation of the pump
will increase the pumping rate, but increased power input is required to a disproportionate,
unfavourable extent. However, the local bursts of acceleration give a substantial
increase in pumping rate, due to the pulsating suction effect at the probe aperture
78, without requiring such a disproportionate increase in power input. For a given
power input, the pumping rate is readily optimised by appropriate selection of the
number of angularly spaced radial protrusions 48 and their spacing from the probe
or probes 70.
[0066] The suction effect is believed to be due, at least in part, to turbulance of the
liquid which is created in the region of the aperture caused by separation of the
liquid from the probe surface at the top of the ramp.
[0067] A preferred pump utilising the last described effect is shown in Figure 5, wherein
the same references are employed for parts similar to the embodiment of Figures 2,
3 and 4.
[0068] In order to reduce drag effects caused by the stem 50 or radial struts 79, the wing-shaped
probe 70 is carried by a supporting disc 82. With such an arrangement, resistive drag
effects can be reduced by positioning the disc 82 adjacent one axial end face 84 of
the housing 10, and providing a guard disc 86 carried by the housing adjacent the
opposite side of the supporting disc. The plate like surfaces 84 and 86 define narrow
spacings against each face of the supporting disc, within which, at least in the region
of the outer periphery of the disc within the operational liquid annulus, a thin film
of liquid is contained. In theory the thickness of each such liquid film should be
just sufficient to contain two boundary layers of the liquid, which, when the housing
is rotating relative to the supporting disc, are able to move past one another with
a minimum shearing effect. Although a residual resistive drag effect remains, the
total resistance is reduced. This is because the major part of the drag resistance
is created by turbulance in the adjacent liquid created by the relative circular motion.
In a restricted space adjacent the supporting disc, an insufficient thickness of liquid
is contained to permit turbulant paths of motion to be created and thus a major part
of the normally experienced drag resistance can be avoided.
[0069] In practice it is difficult to achieve the theoretical ideal mentioned above since
the boundary layer thicknesses will vary with radius and temperature for any given
fluid and speed of rotation. In practice it has been found sufficient to reduce the
gap between the annular sufaces when using conventional vacuum oil to approximately
1 mm and similar considerations would appear to apply when other working liquids are
used.
[0070] As exemplified by Figure 5, the guard disc 86 is mounted to the housing 10 by a mounting
tube 88 apertured at 90 to enable air, gas or other fluid to be pumped to pass into
the central region of the pump. Figure 5 also shows the rotating housing 10 sealing
to the hub 44 by means of a triangular section seal 92, thereby to reduce friction,
and the inlet passage 54 to the probe and the outlet passage 58 from the pump passing
through said hub.
[0071] Figure 6 shows a modification of the embodiment of Figure 5, wherein the probe supporting
disc 82 is positioned at the axial centre of the housing 10. In this instance, two
rotating guard discs 94 and 96 are provided, one adjacent each face of the supporting
disc 82.
[0072] It is to be understood that although only one wing-like probe 70 is shown in each
of Figures 5 and 6, two or more such probes 70 may be circularly spaced around the
periphery of the disc support 82, with ports 54 interconnecting the different apertures
78 to the inlet.
[0073] Protrusions of varying cross sectional shape have been shown in the pumps illustrated
in the drawings. Experimental evidence indicates that the cross sectional shape of
the protrusions which cooperate with the aperture containing surface(s) of the probe(s)
has a considerable effect on the pumping speed (i.e throughput) and the ultimately
achievable vacuum, when using any given pump.
[0074] Examples of two cross sectional shapes which have worked reasonably well are shown
in Figs 2 and 4. In the first case the cross sectional shape can be likened to a quadrant
of a circle and in the second case the shape is generally semi-circular.
[0075] As shown in Fig 2 the curved face of each protrusion constitutes the trailing edge
as viewed by the probe. Experiments have revealed that the opposite orientation of
this quadrant-like cross sectional shape may produce better performance, ie. with
the curved faces now seen as the leading edges of the protrusions as viewed from the
probe.
[0076] Other cross sectional shapes which have been employed are triangular section protrusions
and good results were also obtained.
[0077] Experimental evidence to date suggest that further improvements might be obtained
by using protrusions in the form of generally radially directed blades. The expression
"generally radially directed" includes blades which extend from the part of the pump
on which they are mounted both in a true radial direction and blades which are inclined
to the true radial direction either in the direction of rotation or opposite thereto.
The blades may be straight when viewed from one end, or may be curved convexly or
concavely or in a complex manner.
[0078] Generally the protrusions will extend as shown in the example radially either inwardly
from the housing or outwardly from a central hub (as in Fig 1), but when the suction
aperture(s) is/are located in a radially extending external probe surface, the protrusions
need to extend in an axial sense, at least in part, so at to cooperate therewith.
[0079] The rotatable part of any of the pumps so far described may be driven by an electric
motor or other drive unit. However, where the liquid is either magnetic, magnetisable
or conductive and the housing is of a material which does not significant interfere.with
a magnetic flux field, the housing and other pump parts may remain stationary and
the relative rotation may be effected by influencing the liquid with a rotating magnetic
flux as described in relation to Figure 4. Such a rotating magnetic field may be utilised
alone or in conjunction with rotation by an electric motor or other drive unit.
[0080] When a pump such as described in Figures 3 to 5 is mounted directly on a motor, it
will be appreciated that the housing can be directly attached to the motor shaft and
the hub fixed to the motor frame. All that is required (see Figures 5 and 6) is an
annular seal such as of rubber, synthetic rubber or PTFE between the housing and the
hub. Bearings are not required.
[0081] In a multistage line of pumps, connected outlet to inlet in a series, the connections
are preferably made near the centre line of the housings, thus enabling filling with
working liquid from one end, provided that at least one probe in each pump stage is
downwardly directed during such a filling operation to enable liquid passage from
one housing to the next via each such probe.
[0082] Also, as is conventional in a single or multistage pump, an anti-suck back valve
or reservoir may be fitted at the inlet when the pump is to be used in the suction
mode.
[0083] Typical speeds of operation may be 750, 1500 or 3000 RP
M in accordance with normal operating speeds of synchronous machines. In the case of
Figure 5 or Figure 6 embodiment, for example, a pump operating at 3000 r.p.m would
require a supporting disc diameter of the order of 12 cm.
1. A pump comprising a pump housing having a generally cylindrical surface and enclosing
a quantity of a working liquid, at least one suction device having a passage for communicating
with a first external space, means for causing the liquid to move in a circular path
inside the housing to traverse said device and thereby draw fluid to be pumped therefrom,
and outlet means for communicating a second external space with a central region of
the housing which in use is liquid-free:
characterised in that:
said device comprises a probe (12, 52 or 70) having at least one aperture (28, 56
or 78) in an external surface thereof over which the liquid flows in use and through
which fluid can be sucked from an internal passage in the probe communicating therewith,
to pass as fluid bubbles into said liquid (14) towards the liquid-free central region
as a result of the centrifugal forces acting on the more dense liquid, the bubbles
migrating through the circulating liquid into the central region to pass out of the
housing (10) through the outlet means (26 or 5b).
2. A pump as claimed in claim 1, characterised in that the probe is carried by one
of two relatively rotating inner and outer parts, of which the housing constitutes
the outer part, and the liquid is caused to move in its circular path by the rotation
of the other said part.
3. A pump as claimed in claim 2, characterised in that said other part carries angularly
spaced protrusions which in use pass sufficiently close to the probe to cause short
bursts of acceleration of the region of liquid local to the probe as said liquid is
squeezed between the probe and the protrusion passing thereby, in order to enhance
suction at the probe aperture.
4. A pump as claimed in claim 3, characterised in that the spacing apart of the protrusions
and their spacing from the probe is optimised to maximise fluid drawn through the
probe as a result of the bursts in acceleration for a given power input for driving
the relatively rotating parts of the pump.
5. A pump as claimed in claim 2 or in claim 3 or claim 4 when appendant to claim 2,
characterised in that the probe is supported by a stationary disc within the pump
housing and the latter constitutes the rotating part of the pump.
6. A pump as claimed in claim 5, characterised in that the faces of the supporting
disc are narrowly spaced from respective plate surfaces wherein thin liquid films
are contained.
7. A pump as claimed in claim 6, characterised in that one face of the supporting
disc is spaced from one end face of the housing by one said liquid film and the other
face of the disc is spaced by said liquid film from a guard disc mounted to rotate
with the housing.
8. A pump as claimed in claim 7, characterised in that the mounting of the guard disc
is apertured to provide for passage of fluid to the central region of the housing.
9. A pump as claimed in any of claims 1 to 8, characterised in that the probe is in
the form of a wing extending parallel to the pump axis.
10. A pump as claimed in claim 9, characterised in that the wing has a ramp surface
-at the leading edge of the wing preceding the aperture or apertures.
11. A pump according to claim 10, characterised by at least one ridge or protrusion
in the surface of the ramp which serves to disturb the flow of liquid thereover.
12. A pump according to claim 1 or any claim dependant thereon, wherein means is provided
to produce a rotating magnetic flux field and the liquid is either magnetic or magnetisable
or electrically conductive and is made to circulate so as to form a liquid annulus
under the influence of the rotating magnetic flux field.
13. A method of pumping a fluid from one region to another by employing a suction
effect created by the interaction of a liquid which is more dense than the fluid to
be pumped, and orifice means, wherein the less dense fluid is entrained into the more
dense liquid, the latter is caused to follow a curved path so as to introduce centrifugal
forces therein and thereby produce radial separation of the liquid and the less dense
fluid entrained therein and wherein the displaced fluid is conveyed to the said other
region after separation,
characterised by the step of:
causing the liquid to flow over and in contact with an exterior surface containing
the said orifice to create a pressure drop in the liquid in the region of the orifice
and thereby draw fluid from the said one region into the working liquid moving across
the orifice.